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You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:B
[texts]Behavior of fast moving flow of compressible gas in cylindrical pipe in presence of cooling : = K voprosu o povedenii bystrodvizhushchegosya potoka szhimaemogo gaza v pryamoi tsilindricheskoi trube pri nalichii okhlzahdenia - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003689748&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Aeronautics
Downloads: 97
[texts]Behavior of the laminar boundary layer for periodically oscillating pressure variation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759951&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 172
[texts]Belt method for measuring pressure distribution - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805095&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 95
[texts]Boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875156&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Boundary layer--Research
Downloads: 93
[texts]Boundary layers in fluids with little friction : = Grenzschichten in flüssigkeiten mit kleiner reibung - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003690109&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Turbulent boundary layer
Downloads: 183
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